LWK 79-100 (lwk79100-il) Xfoil prediction polar at RE=50,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: LWK 79-100 (lwk79100-il) Reynolds number: 50,000 Max Cl/Cd: 25.9 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-lwk79100-il-50000.txt Download as CSV file: xf-lwk79100-il-50000.csv |
XFOIL Version 6.96
Calculated polar for: LWK 79-100
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.050 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 -0.7269 0.09239 0.08554 0.0032 1.0000 0.1681
-9.250 -0.7081 0.08803 0.08113 0.0047 1.0000 0.1647
-9.000 -0.8013 0.07137 0.06439 -0.0110 1.0000 0.1389
-8.750 -0.8086 0.06569 0.05854 -0.0123 1.0000 0.1382
-8.500 -0.8135 0.06016 0.05273 -0.0132 1.0000 0.1376
-8.250 -0.8157 0.05481 0.04696 -0.0136 1.0000 0.1377
-8.000 -0.8120 0.04983 0.04144 -0.0136 1.0000 0.1381
-7.750 -0.8029 0.04534 0.03630 -0.0131 1.0000 0.1393
-7.500 -0.7824 0.04250 0.03354 -0.0125 1.0000 0.1465
-7.250 -0.7675 0.03910 0.02947 -0.0118 1.0000 0.1528
-7.000 -0.7456 0.03614 0.02641 -0.0111 1.0000 0.1597
-6.750 -0.7247 0.03361 0.02356 -0.0103 1.0000 0.1713
-6.500 -0.7019 0.03133 0.02108 -0.0095 1.0000 0.1853
-6.250 -0.6782 0.02924 0.01900 -0.0087 1.0000 0.2034
-6.000 -0.6554 0.02732 0.01710 -0.0076 1.0000 0.2298
-5.750 -0.6333 0.02554 0.01553 -0.0064 1.0000 0.2659
-5.500 -0.6129 0.02401 0.01431 -0.0048 1.0000 0.3158
-5.250 -0.5936 0.02292 0.01366 -0.0026 1.0000 0.3771
-5.000 -0.5746 0.02244 0.01361 0.0003 1.0000 0.4431
-4.750 -0.5552 0.02259 0.01404 0.0038 1.0000 0.5036
-4.500 -0.5354 0.02297 0.01458 0.0075 1.0000 0.5546
-4.250 -0.5159 0.02322 0.01486 0.0114 1.0000 0.5994
-4.000 -0.4973 0.02318 0.01481 0.0149 1.0000 0.6409
-3.750 -0.4782 0.02312 0.01477 0.0188 1.0000 0.6755
-3.500 -0.4596 0.02285 0.01449 0.0224 1.0000 0.7090
-3.250 -0.4410 0.02248 0.01406 0.0258 1.0000 0.7410
-3.000 -0.4213 0.02207 0.01362 0.0288 1.0000 0.7712
-2.750 -0.3989 0.02167 0.01318 0.0313 1.0000 0.8002
-2.500 -0.3715 0.02132 0.01278 0.0328 1.0000 0.8286
-2.250 -0.3354 0.02105 0.01239 0.0325 1.0000 0.8566
-2.000 -0.2882 0.02086 0.01207 0.0298 1.0000 0.8841
-1.750 -0.2304 0.02066 0.01170 0.0246 1.0000 0.9108
-1.500 -0.1496 0.02037 0.01121 0.0146 1.0000 0.9346
-1.250 -0.0876 0.01983 0.01057 0.0072 1.0000 0.9571
-1.000 -0.0237 0.01913 0.00983 -0.0011 1.0000 0.9777
-0.750 0.0386 0.01836 0.00905 -0.0096 1.0000 0.9977
-0.500 0.0522 0.01804 0.00884 -0.0099 1.0000 1.0000
-0.250 0.0407 0.01805 0.00896 -0.0068 1.0000 1.0000
0.000 0.0000 0.01822 0.00916 0.0000 1.0000 1.0000
0.250 -0.0407 0.01805 0.00896 0.0068 1.0000 1.0000
0.500 -0.0521 0.01804 0.00883 0.0099 1.0000 1.0000
0.750 -0.0387 0.01836 0.00905 0.0097 0.9978 1.0000
1.000 0.0237 0.01913 0.00982 0.0011 0.9778 1.0000
1.250 0.0874 0.01982 0.01056 -0.0071 0.9571 1.0000
1.500 0.1495 0.02037 0.01120 -0.0146 0.9347 1.0000
1.750 0.2305 0.02066 0.01170 -0.0246 0.9108 1.0000
2.000 0.2883 0.02085 0.01206 -0.0298 0.8840 1.0000
2.250 0.3354 0.02105 0.01239 -0.0325 0.8566 1.0000
2.500 0.3715 0.02132 0.01277 -0.0328 0.8286 1.0000
2.750 0.3989 0.02167 0.01318 -0.0313 0.8003 1.0000
3.000 0.4213 0.02207 0.01362 -0.0288 0.7712 1.0000
3.250 0.4410 0.02248 0.01406 -0.0258 0.7409 1.0000
3.500 0.4596 0.02285 0.01449 -0.0224 0.7090 1.0000
3.750 0.4781 0.02312 0.01477 -0.0188 0.6755 1.0000
4.000 0.4973 0.02318 0.01481 -0.0149 0.6409 1.0000
4.250 0.5159 0.02322 0.01486 -0.0113 0.5994 1.0000
4.500 0.5354 0.02297 0.01458 -0.0075 0.5545 1.0000
4.750 0.5552 0.02259 0.01404 -0.0037 0.5036 1.0000
5.000 0.5746 0.02244 0.01361 -0.0003 0.4431 1.0000
5.250 0.5936 0.02292 0.01366 0.0026 0.3771 1.0000
5.500 0.6129 0.02400 0.01431 0.0048 0.3158 1.0000
5.750 0.6333 0.02554 0.01553 0.0064 0.2659 1.0000
6.000 0.6555 0.02732 0.01710 0.0076 0.2297 1.0000
6.250 0.6782 0.02925 0.01900 0.0087 0.2033 1.0000
6.500 0.7020 0.03133 0.02109 0.0095 0.1853 1.0000
6.750 0.7248 0.03360 0.02355 0.0103 0.1711 1.0000
7.000 0.7457 0.03614 0.02641 0.0111 0.1596 1.0000
7.250 0.7676 0.03911 0.02948 0.0118 0.1528 1.0000
7.500 0.7825 0.04250 0.03354 0.0125 0.1464 1.0000
7.750 0.8030 0.04536 0.03632 0.0131 0.1392 1.0000
8.000 0.8121 0.04985 0.04145 0.0136 0.1381 1.0000
8.250 0.8158 0.05484 0.04698 0.0136 0.1377 1.0000
8.500 0.8139 0.06018 0.05275 0.0131 0.1376 1.0000
8.750 0.8077 0.06577 0.05863 0.0121 0.1380 1.0000
9.000 0.8011 0.07140 0.06442 0.0109 0.1388 1.0000
9.250 0.6017 0.10850 0.10124 -0.0331 0.3378 1.0000
|
Polar data table (+)
Polar graphs
<< Back to LWK 79-100 (lwk79100-il)